TELE-TECH & - AmericanRadioHistory.Com
TELE-TECH & - AmericanRadioHistory.Com
TELE-TECH & - AmericanRadioHistory.Com
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Um OALOHM... ntiltiatune gut nw.<br />
You can depend on 4<br />
TYPE RH<br />
MINIATURE POWER RESISTORS<br />
For all applications where the equipment must survive<br />
the most severe environmental, shock, vibration, humidity<br />
and temperature conditions.<br />
Smallest in size; completely welded from terminal to<br />
terminal; silicone sealed in a die -cast black anodized<br />
aluminum housing and mounts on sub -panel for maximum<br />
heat dissipation; impervious to moisture, salt<br />
ions, vapor and gases.<br />
Three wattage ranges: RH -25, 25 watts;<br />
RH -50, 50 watts; RH -250, 250 watts.<br />
Temperature coefficient 0.00002 /Deg. C<br />
Ranges from 0.1 ohm to 55,000 ohms,<br />
depending on type<br />
Tolerances 0.05 %, 0.1 %, 0.25 %,<br />
0.5 %, 1 %, 3 %, 5%<br />
Conform to applicable JAN and MIL Specifications<br />
Write for Bulletin R -21 -6<br />
DALE PRODUCTS, INC_<br />
Phone 2139<br />
1304 28th Ave. Columbus, Nebraska, U.S.A.<br />
<strong>TELE</strong>METRY<br />
E<br />
At RREP, systems engineering<br />
assumes paramount importance.<br />
<strong>Com</strong>ponent and assembly design<br />
are examined critically, always<br />
in relationship to the overall<br />
system. And unique building<br />
block design permits individual<br />
components and assemblies to<br />
be package engineered into form<br />
iU<br />
Export Dept t<br />
Pan -Mar Corp.,<br />
1270 Broadway<br />
New York 1, N.<br />
In Canada:<br />
Charles W. Pointen, Ltd.<br />
6 Alcin° Ave., Toronto<br />
SYSTEMS<br />
WI HETHIE G<br />
CREATIVE<br />
SPARK<br />
factors to fulfill a wide variety<br />
of applications.<br />
It is no accident that U. S. military<br />
agencies, foreign governments,<br />
most aircraft companies<br />
and many research and industrial<br />
organizations specify RREP<br />
telemetric data transmitting systems<br />
for reliability under extreme<br />
operating conditions.<br />
CREATIVE ENGINEERING IS THE DIFFERENCE!<br />
Technical bulletins describing RREP's complete line<br />
of telemetering equipment available upon request.<br />
RREP Type 1001A Crystal Controlled Transmitter.<br />
RF power output: 3.5 to 4.5 watts into<br />
52 -ohm load. Frequency range: 215 to 235 megacycles.<br />
Frequency stability: ±0.005 %.<br />
1111E15<br />
RAYMOND ROSEN<br />
ENGINEERING PRODUCTS, INC.<br />
32nd & Walnut Streets, Philadelphia 4, Pennsylvania<br />
15106 Ventura Boulevard, Sherman Oaks, California<br />
Finned Magnetron<br />
(Continued from page 174)<br />
were built and tested. The dummy<br />
magnetron used for the tests with<br />
the various cooling fins employed<br />
a coiled nichrome wire heater,<br />
housed within a simulated anode<br />
block, and a r -f output pipe connected<br />
to the simulated anode block<br />
(see Fig. 2). The test equipment<br />
consisted of a positive displacement<br />
blower supplying air, metered by a<br />
rotameter, to a plenum chamber;<br />
the air passed from the plenum<br />
chamber through a transition piece<br />
into the magnetron.<br />
For each set of cooling fins, temperature<br />
and pressure drop characteristics<br />
were obtained over a<br />
range of airflows. In all cases fin<br />
thickness was .030 in., with .080 in.<br />
between fins; overall fin length and<br />
width were approximately 3 x 31/2<br />
in. for all fins except the original<br />
fin (Fig. 3) which was approximately<br />
21/2 in. sq. Inlet air temperature<br />
was 30 °C. The location of<br />
the hot spot temperature tx,,,,px is<br />
shown in Fig. 2.<br />
A typical curve of (tc,n,ax tt,Inlet)<br />
and pressure drop as a function of<br />
airflow is given in Fig. 4 for the<br />
set of original fins (Fig. 3). All 4<br />
types of fin modifications, shown in<br />
Figs. 5, 6 and 7, gave substantial<br />
improvements over this original design.<br />
Fig. 5 shows the first modification,<br />
a fin with deflector vanes. The<br />
purpose of the vanes was to force<br />
more air to flow over the output<br />
pipe, since the pipe temperature is<br />
close to the anode temperature and<br />
the pipe conducts much of the heat<br />
away from the anode. It was<br />
thought this would cause an increase<br />
in local h at this region for<br />
any given flow, and therefore demand<br />
less air to achieve the overall<br />
hS product required. The dummy<br />
magnetron with a set of this type<br />
of fins required only 29 cfm and 2.8<br />
in. of water to have a satisfactory<br />
hS value.<br />
An improvement over the fin of<br />
Fig. 5 was considered possible by<br />
deflecting all of the air more<br />
gradually over the outlet pipe,<br />
thereby increasing h locally, and<br />
reducing the loss associated with<br />
the turning. This could be ac-<br />
(Continued on page 178)<br />
176 For product information, use inquiry cord on pages 209 -210 Tele -Tech & ELECTRONIC INDUSTRIES June 1956